Mission type | Earth observation Technology |
---|---|
Operator | ASI |
COSPAR ID | 2019-015A |
SATCAT no. | 44072 |
Website | prisma-i |
Mission duration | 5 years (planned) 5 years, 8 months and 2 days (elasped) |
Spacecraft properties | |
Manufacturer | Leonardo OHB Italia |
Launch mass | 830 kilograms (1,830 lb) |
Dimensions | 1.75 m x 1.54 m x 3.4 m |
Power | 350 W (avg.) 700 W (max) |
Start of mission | |
Launch date | 22 March 2019, 01:50:35UTC[1] |
Rocket | Vega[2] |
Launch site | Kourou ELV |
Contractor | Arianespace |
Orbital parameters | |
Reference system | Geocentric |
Regime | Sun-Synchronous Orbit |
Eccentricity | 0 |
Apogee altitude | 614 km (382 mi) |
Inclination | 98.19 degrees |
Period | 99 minutes |
Mean motion | 15 |
Repeat interval | 29 days |
Epoch | Planned |
Transponders | |
Band | S Band (tracking/control) X band (data transmission) |
Frequency | 9.6 GHz |
Bandwidth | 155 Mbit/s |
PRISMA (PRecursore IperSpettrale della Missione Applicativa,[2] Hyperspectral PRecursor of the Application Mission) is an Italian Space Agency pre-operational and technology demonstrator mission focused on the development and delivery of hyperspectral products and the qualification of the hyperspectral payload in space.[3]